CN106494651A - A kind of non-firer's separator of low impact - Google Patents

A kind of non-firer's separator of low impact Download PDF

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Publication number
CN106494651A
CN106494651A CN201611039566.0A CN201611039566A CN106494651A CN 106494651 A CN106494651 A CN 106494651A CN 201611039566 A CN201611039566 A CN 201611039566A CN 106494651 A CN106494651 A CN 106494651A
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CN
China
Prior art keywords
locking sleeve
housing
separator
ball
firer
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Pending
Application number
CN201611039566.0A
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Chinese (zh)
Inventor
冯伟
冀娟
傅俊勇
曾凡铨
胡翔宇
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Shanghai Aerospace Control Technology Institute
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Shanghai Aerospace Control Technology Institute
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Priority to CN201611039566.0A priority Critical patent/CN106494651A/en
Publication of CN106494651A publication Critical patent/CN106494651A/en
Pending legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/645Separators

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  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Forms Removed On Construction Sites Or Auxiliary Members Thereof (AREA)

Abstract

A kind of non-firer's separator of low impact, between rocket level, between the satellite and the rocket, the locking of satellite sun windsurfing and antenna etc. and release, using marmem as trigger switch, and be equipped with the parts such as spring, locking sleeve, point lobe nut and constitute.SME based on marmem, tensile pre-deformation is first carried out to which during assembling, when needing to separate unblock, to alloy material electrified regulation to its phase transition temperature, make it restore to the shape before predeformation, and then triggering block action is driven, locking sleeve is disengaged with point lobe nut, realize the release of the load such as satellite.After first separation is completed, it is convenient to take out the trigger part of enclosure interior, shape-memory alloy wire is carried out again to load after predeformation using special tooling, you can reuse.The separator of the present invention impacts low, reusable, pollution-free, low cost, uses safety, is particularly suited for separately impacting the occasion having high demands.

Description

A kind of non-firer's separator of low impact
Technical field
The present invention relates to spacecraft locking separation technology field, non-firer's separator of more particularly to a kind of low impact.
Background technology
With the development of the technology such as micro & nano technology, integrated multi-functional structure, integrated integrated electronicses, spacecraft precise treatment Trend is more obvious, such as the development and application of microsatellite, just progressively substitutes some space tasks of traditional large satellite.With space flight Device precision, the raising of integration degree, require to the separation impact similar to accurate spacecraft as microsatellite more next More harsh.The at present domestic separator that adopts is substantially firer's separator, but its impact for producing big (3000g~ 5000g), the damage or misoperation of peripheral parts is easily caused, affects to separate reliability, be difficult to be suitable for precision spacecraft or which is attached The separation of category part.Meanwhile, there is the shortcomings of inflammable and explosive, inconvenient storage, transport and operation, safety in utilization in firer's separator Difference;Belong to running stores, not reproducible use, reliability are difficult to verify;A certain proportion of sample need to be extracted from batch product Product do blasting test to verify batch qualification rate, certainly will increase cost.In consideration of it, the separator of low impact is in space industry Application demand is more and more strong.
Content of the invention
The technical problem to be solved in the present invention is:The deficiencies in the prior art, the present invention are overcome to provide a kind of the non-of low impact Firer's separator, low impact, the separator of reusable, pollution-free, safe, low cost, so that meet space flight Device and its special of associate member separate demand, improve and separate reliability and security.
The technical solution adopted in the present invention is:A kind of non-firer's separator of low impact, including marmem Silk, triggering block, point lobe nut, locking sleeve, compression spring, safety spring, buffer spring, ball, ball baffle ring, steel ball, shell Body, end cap, upper bracket, lower carriage;Upper bracket is located in housing, on lower carriage, is formed between upper bracket and lower carriage Cavity, triggering block is in cavity;After shape-memory alloy wire doubling, doubling end is fixed in triggering block, and leading-out terminal is passed through Upper bracket end face middle through-hole is separately fixed on upper bracket end face, and safety spring is arranged between upper bracket and triggering block, is carried Make shape-memory alloy wire exceptionally straight for tension force;Lower carriage end flange is stuck at inner walls ledge structure, other end insertion lock In tight sleeve, locking sleeve intermediate membrane side is located at, buffer spring is enclosed within lower carriage outer wall, one end and lower carriage end method Blue connection, the other end are connected with locking sleeve one end end;The locking sleeve other end is against on housing end face, in housing; Compression spring is enclosed within locking sleeve outer wall, and one end is against on locking sleeve outer wall ledge structure, and the other end is against housing end face On;Steel ball inlay card in locking sleeve inboard wall groove and lower carriage lateral through aperture and is against triggering block outer wall, and triggering block is not installed Spring one end side wall has the groove coordinated under released state with steel ball;Lobe nut is divided to be located at locking sleeve intermediate membrane opposite side, Bolt passes through housing end face center, end to be arranged in point lobe nut, in the center of locking sleeve intermediate membrane, housing end face The bulge-structure of wall center is inserted point lobe nut two ends respectively and is coordinated with point lobe nut inner hole;Ball baffle ring is enclosed within locking sleeve On, ball is embedded in locking sleeve sidewall notches, is against ball baffle ring inwall on the outside of ball, and inner side is against a point lobe nut side Wall, a point lobe nut side wall have the groove under released state with ball engagement;End cap is arranged on shell nozzle end.
The buffer spring at the locking sleeve two ends and compression spring are compressive state, and the tension force of compression spring is more than slow Spring is rushed, and locking sleeve support motion upwards is driven when shape-memory alloy wire is triggered.
The material of the shape-memory alloy wire is Nitinol.
Coordinated by standard thread between described point of lobe nut and bolt.
The housing is hexa-prism cylinder or cylindrical drum, and one end open, the other end have end face;Housing is near bolt There is flange mounting surface one end.
Present invention advantage compared with prior art is:
(1) igniter module that the present invention is made up of shape-memory alloy wire 10 and triggering block is the core of the present invention Part, shape-memory alloy wire before separator is loaded have carried out pre-tension deformation process by special tooling to which, can facilitate Realize reusing in ground.
(2) of the invention when separator is in locking state, by between compression spring, safety spring, buffer spring Dynamic balance and the inlay card of steel ball, it is ensured that locking sleeve position is fixed, so as to a point lobe nut radial constraint, make bolt with a point lobe spiral shell In effectively connection state, mother realizes that the reliability to load is locked.
(3) of the invention when separator will be unlocked and be separated, by heating to shape-memory alloy wire so as to quick liter Temperature because the material has SME, can return to original shape to more than phase transition temperature, so as to drive triggering block to transport Dynamic, make steel ball, ball be embedded in succession relevant position, release the radial constraint of point lobe nut, bolt is separated with a point lobe nut, Can achieve to efficiently separate load.
(4) present invention is after first separation is completed, it is convenient to by the upper bracket of enclosure interior, lower carriage, safe bullet Spring, triggering block, shape-memory alloy wire integrally take out, and shape-memory alloy wire are carried out after predeformation again using special tooling Load, can achieve to reuse.
(5) present invention is suitable for the separation trigger signal types of spacecraft standard, and reaches equal with firer's separator Technical indicator, concurrently separate impact little (within 500g), (no less than 20 times) can be repeatedly used;May be used on all kinds of boats The locking of its device and its associate member and separate, such as rocket, manned spaceship, satellite, solar array, antenna etc., while can promote Civil area is applied to, and is limited because trigger not being separated by spacecraft standard, can be according to specific interface requirement and use Require, adjust corresponding index.
Description of the drawings
The non-firer's separator construction profile figures of Fig. 1;
Non- firer's separator section of structure under Fig. 2 locking states;
Non- firer's separator section of structure under Fig. 3 released states;
The non-firer's separators of Fig. 4 repeat predeformation schematic diagram.
Specific embodiment
As shown in Fig. 1~Fig. 2, the present invention provides a kind of non-firer's separator of low impact, and the separator is by shape Memory alloy wire 10, triggering block 11, point lobe nut 6, locking sleeve 12, compression spring 5, safety spring 2, buffer spring 3, ball 13rd, ball baffle ring 14, steel ball 4, housing 8, end cap 7, upper bracket 1, lower carriage 2 are constituted, and structure composition figure is as shown in Figure 2.
Housing 8 is flange mounting surface near one end of bolt 15, before bolt 15 is connected with non-firer's separator, can be by Non- firer's separator is fixed on place to be installed;Upper bracket 1 is located in housing 8, on lower carriage 9, upper bracket 1 and lower Cavity is formed between frame 9, and triggering block 11 is in cavity;After 10 doubling of shape-memory alloy wire, doubling end is fixed on triggering On block 11, leading-out terminal is separately fixed on 1 end face of upper bracket through 1 end face middle through-hole of upper bracket, and safety spring 2 is installed in upper Between support 1 and triggering block 11, there is provided tension force makes shape-memory alloy wire 10 exceptionally straight;9 end flange of lower carriage is stuck in housing 8 At wall stand stage structure, in other end insertion locking sleeve 12,12 intermediate membrane side of locking sleeve is located at, buffer spring 3 is enclosed within On 9 outer wall of lower carriage, one end is connected with 9 end flange of lower carriage, and the other end is connected with 12 one end end of locking sleeve;Lock sleeve 12 other ends of cylinder are against on 8 end face of housing, and locking sleeve 12 is located in housing 8;Compression spring 5 is enclosed within 12 outer wall of locking sleeve On, one end is against on 12 outer wall ledge structure of locking sleeve, and the other end is against on 8 end face of housing;4 inlay card of steel ball is in locking sleeve In 9 lateral through aperture of 12 inboard wall grooves and lower carriage and with 11 wall contacts of triggering block, triggering block 11 do not install spring one end side wall There is the groove coordinated under released state with steel ball 4;Lobe nut 6 is divided to be located at 12 intermediate membrane opposite side of locking sleeve, bolt 15 is worn 8 end face center of housing is crossed, end is arranged in point lobe nut 6, in the center of 12 intermediate membrane of locking sleeve, 8 end face of housing The bulge-structure of wall center inserts point 6 two ends of lobe nut respectively with point 6 inner hole of lobe nut;Ball 13 is embedded in locking sleeve In 12 sidewall notches, ball baffle ring (14) inwall on the outside of ball (13), is against, inner side is against 6 side wall of point lobe nut, point lobe spiral shell Female 6 side walls have the groove coordinated under released state with ball 13;End cap 7 is arranged on 8 openend of housing.Housing 8 is hexa-prism Cylinder, one end open, the other end have end face.External equipment is connected with the separator of the present invention by bolt 15, after unblock, spiral shell Bolt 15 is separated with a point lobe nut 6, and external equipment is realized separating.
The material of shape-memory alloy wire 10 is NiTi (NiTi) alloy, and the material has good SME, Material memory strain reachable 8%.
One end of shape-memory alloy wire 10 is fixed in triggering block 11, and the other end (leading-out terminal) is fixed on upper bracket 1, Safety spring 2 is arranged between upper bracket 1 and triggering block 11, there is provided tension force makes shape-memory alloy wire 10 exceptionally straight, and prevents from touching Send out 11 axial float of block and misread lock.Inlay card, in 12 corresponding groove of lower carriage 9 and locking sleeve, constrains lock to steel ball 4 simultaneously Tight sleeve 12 does not produce axially-movable.The buffer spring 3 at 12 two ends of locking sleeve and compression spring 5 are compressive state, compression The tension force of spring 5 can drive locking sleeve 12 to move upwards more than buffer spring 3 when trigger is triggered.Ball 13 is embedded in lock In 12 corresponding groove of tight sleeve, constraint point lobe nut 6 does not produce radial motion.
Shape-memory alloy wire 10 has carried out pre-tension deformation process before separator is loaded so as to reach preboarding Shape, then completes the assembling of separator.When separator is in locking state (Fig. 2), safety spring 3 and compression spring 5 Tension force and steel ball 4 inlay card ensure locking sleeve 12 be fixed on constant position.Locking sleeve 12 passes through 13 pairs of points of lobe spiral shells of ball Female 6 radially exert a force, and make that point lobe nut 6 is effective with bolt 15 to be engaged, locking of the realization to load.
As shown in figure 3, before separator will unlock separation, by heating to shape-memory alloy wire 10 so as to fast Speed is warmed up to more than phase transition temperature, and now shape-memory alloy wire 10 axially contracts deformation, drives triggering block 11 to move upwards, After moving to certain position, steel ball 4 can be slipped in the groove of triggering block 11.Now locking sleeve 12 is unlocked.Locking sleeve 12 is received The thrust of compression spring 6 and move upwards, and drive ball 13 to move upwardly together, ball 13 is embedded in after moving to certain position Divide in the groove of lobe nut 6, point lobe nut 6 power radially is applied to by locking sleeve 12 and ball 13 now and is disappeared, point lobe Nut 6 is disengaged by outer tension force, so that a point lobe nut 6 is departed from bolt 15, and then realizes the separation to load.
As shown in figure 4, after separation is complete, by end cap 7 is dismantled, it is convenient to by upper bracket 1, lower carriage 9 together with Shape-memory alloy wire 10, triggering block 11 in which, 2 overall taking-up of safety spring, as shown in Figure 4.By the pre- of particular design Stretching tool carries out predeformation to shape-memory alloy wire 10, after completing predeformation, the part is reloaded in housing, you can Realize reusing.
Separator of the present invention using shape-memory alloy wire 10 as trigger switch, imitate by the shape memory based on the material Should, carry out pre-treatment before assembly to the material, before unblock is separated, by heating to which so as to reach phase transition temperature, produce Raw deformational displacement, and then drive 12 axially-movable of triggering block, it is recessed in triggering block 12 to be that the steel ball 4 being embedded in retainer 9 is slipped into In groove, and then move axially locking sleeve 12, while drive ball 13 to move, and the corresponding recesses slipped on point lobe nut 6 In, make point lobe nut 6 radially decoupled, realize that the separation to load discharges.
The separator of the present invention can be repeatedly used, after first separation is completed, it is convenient to by enclosure interior Trigger part (i.e. by upper bracket 1, lower carriage 9, safety spring 2, triggering block 11, shape-memory alloy wire 10 constitute whole Body) take out, shape-memory alloy wire 10 is carried out again to load after predeformation using special tooling, you can reuse.
Unspecified part of the present invention belongs to technology as well known to those skilled in the art.

Claims (5)

1. non-firer's separator of a kind of low impact, it is characterised in that including shape-memory alloy wire (10), triggering block (11) lobe nut (6), locking sleeve (12), compression spring (5), safety spring (2), buffer spring (3), ball (13), rolling, are divided Pearl baffle ring (14), steel ball (4), housing (8), end cap (7), upper bracket (1), lower carriage (9);Upper bracket (1) is located at housing (8) Interior, on lower carriage (9), cavity between upper bracket (1) and lower carriage (9), is formed, triggering block (11) is in cavity; After shape-memory alloy wire (10) doubling, doubling end is fixed in triggering block (11), and leading-out terminal is through in the middle part of upper bracket (1) end face Through hole is separately fixed on upper bracket (1) end face, and safety spring (2) is arranged between upper bracket (1) and triggering block (11), there is provided Tension force makes shape-memory alloy wire (10) exceptionally straight;Lower carriage (9) end flange is stuck at housing (8) inwall ledge structure, another In end insertion locking sleeve (12), locking sleeve (12) intermediate membrane side is located at, buffer spring (3) is enclosed within lower carriage (9) outward On wall, one end is connected with lower carriage (9) end flange, and the other end is connected with locking sleeve (12) one end end;Locking sleeve (12) other end is against on housing (8) end face, in housing (8);Compression spring (5) is enclosed within locking sleeve (12) outer wall, One end is against on locking sleeve (12) outer wall ledge structure, and the other end is against on housing (8) end face;Steel ball (4) inlay card is in locking In sleeve (12) inboard wall groove and lower carriage (9) lateral through aperture and triggering block (11) outer wall is against, triggering block (11) does not install bullet One side wall of spring has the groove coordinated under released state with steel ball (4);Lobe nut (6) is divided to be located at locking sleeve (12) intermediate membrane Opposite side, bolt (15) pass through housing (8) end face center, end in point lobe nut (6), in the middle part of locking sleeve (12) every Point lobe nut (6) two ends are inserted respectively with a point lobe nut in the center of plate, the bulge-structure of housing (8) end face inwall center (6) inner hole;Ball baffle ring (14) is enclosed within locking sleeve (12), and ball (13) is embedded in locking sleeve (12) sidewall notches In, ball baffle ring (14) inwall is against on the outside of ball (13), inner side is against point lobe nut (6) side wall, point lobe nut (6) side wall There is the groove coordinated under released state with ball (13);End cap (7) is arranged on housing (8) openend.
2. a kind of non-firer's separator of low impact according to claim 1, it is characterised in that the locking sleeve (12) buffer spring (3) at two ends and compression spring (5) are compressive state, and the tension force of compression spring (5) is more than buffer spring 3, drive locking sleeve (12) to move to upper bracket (1) when shape-memory alloy wire (10) is triggered.
3. a kind of non-firer's separator of low impact according to claim 1 and 2, it is characterised in that the shape note The material for recalling B alloy wire (10) is Nitinol.
4. a kind of non-firer's separator of low impact according to claim 1 and 2, it is characterised in that described point of lobe spiral shell Coordinated by standard thread between female (6) and bolt (15).
5. non-firer's separator of a kind of low impact according to claim 1 and 2, it is characterised in that housing (8) For hexa-prism cylinder or cylindrical drum, one end open, the other end have end face;Housing (8) has method in the one end near bolt (15) Blue mounting surface.
CN201611039566.0A 2016-11-21 2016-11-21 A kind of non-firer's separator of low impact Pending CN106494651A (en)

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CN113386984A (en) * 2021-08-04 2021-09-14 北京中科宇航技术有限公司 Satellite and rocket separation unlocking driving device
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CN113734474A (en) * 2021-08-09 2021-12-03 北京空间飞行器总体设计部 Method and system for determining outsole separation triggering conditions under multiple constraints
CN113753268A (en) * 2021-09-07 2021-12-07 天津爱思达航天科技有限公司 Star and arrow separation unblock actor
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CN114408223A (en) * 2021-12-21 2022-04-29 兰州空间技术物理研究所 Quick reset buffer device of power adjusting mechanism
CN114408223B (en) * 2021-12-21 2023-08-15 兰州空间技术物理研究所 Quick buffer that returns to normal of power adjustment mechanism
CN114455107A (en) * 2022-03-01 2022-05-10 武汉科技大学 Non-explosive separation device based on SMA connecting piece switch
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CN114750105A (en) * 2022-05-23 2022-07-15 北京微动时空科技有限公司 Pin puller based on memory alloy
CN114771884A (en) * 2022-05-27 2022-07-22 长光卫星技术股份有限公司 Non-firer large-bearing compression release mechanism capable of resetting quickly
CN115231001A (en) * 2022-07-27 2022-10-25 大连理工大学 Radial connection unlocking device for non-firer rocket body and using method
CN115231001B (en) * 2022-07-27 2024-08-09 大连理工大学 Radial connection unlocking device for non-rocket body and use method
CN115723972B (en) * 2022-12-19 2023-09-12 苏州馥昶空间技术有限公司 Compression release mechanism
CN115723972A (en) * 2022-12-19 2023-03-03 苏州馥昶空间技术有限公司 Compressing and releasing mechanism
CN116534289B (en) * 2023-07-05 2023-10-13 北京未来宇航空间科技研究院有限公司 Pneumatic separation system and use method thereof
CN116534289A (en) * 2023-07-05 2023-08-04 北京未来宇航空间科技研究院有限公司 Pneumatic separation system and use method thereof
CN117416534A (en) * 2023-12-19 2024-01-19 四川航天川南火工技术有限公司 Gap-keeping type fire-work-division separation lock device
CN117416534B (en) * 2023-12-19 2024-03-26 四川航天川南火工技术有限公司 Gap-keeping type fire-work-division separation lock device

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Application publication date: 20170315